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Vertically rising aircraft -- Aerodynamics -- Congresses

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• Vertically rising aircraft -- Aerodynamics
• Short take-off and landing aircraft -- Aerodynamics -- Congresses
• Vertically rising aircraft -- Congresses
• Aerodynamics -- Congresses

• Proceedings of a Workshop on V/STOL Aircraft Aerodynamics (Monterey, Calif. : Dept. of the Navy, Naval Postgraduate School, [1979], 1979), by Workshop on V/STOL Aircraft Aerodynamics, M. F. Platzer, C. Henderson, and Naval Air Development Center (page images at HathiTrust; US access only)

Items below (if any) are from related and broader terms.

• Effects of gust velocity spatial distributions on lateral-directional response of a VTOL aircraft (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Directorate of Laboratories, Air Force Systems Command, 1967., 1967), by Robert L. Swaim, Alonzo J. Connors, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Michael A. Boles and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• NASA TN D-2380 (National Aeronautics and Space Administration :, 1964), by Raymond D. Vogler, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
• A Flight evaluation of a vectored-thrust-jet V/STOL airplane during simulated instrument approaches using the Kestrel (XV-6A) airplane (National Aeronautics and Space Administration ;, 1972), by Samuel A. Morello, Richard G. Culpepper, Robert E. Shanks, Lee H. Person, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• An examination of handling qualities criteria for V/STOL aircraft (National Aeronautics and Space Administration :, 1960), by Seth B. Anderson and Ames Research Center (page images at HathiTrust)
• Investigation of the aerodynamic characteristics of a supersonic horizontal- attitude VTOL airplane model at Mach numbers of 1.57, 2.14, 2.54, and 2.87 (National Aeronautics and Space Administration, 1960), by Arthur E. Franklin, Robert M. Lust, and Langley Research Center (page images at HathiTrust)
• Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels (National Aeronautics and Space Administration, 1961), by M. Leroy Spearman, Gerald V. Foster, and Langley Research Center (page images at HathiTrust)
• Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds (National Aeronautics and Space Administration, 1960), by Walter B. Olstad and Langley Research Center (page images at HathiTrust)
• NASA TN D-1802 (National Aeronautics and Space Administration, 1963), by Henry L. Kelley, Robert A. Champine, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range (National Aeronautics and Space Administration :, 1962), by James H. Otis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1965 (National Aeronautics and Space Administration, 1963), by Robert H. Kirby, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Longitudinal and lateral stability characteristics of two four-jet vtol models in the transition speed range (National Aeronautics and Space Administration, 1965), by Raymond D. Vogler, Richard E. Kuhn, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Rotorwash computer model : user's guide (Federal Aviation Administration, Research and Development Service ;, 1992), by Samuel W. Ferguson, J. David Kocurek, Computational Methodology Associates, and United States. Federal Aviation Administration. Research and Development Service (page images at HathiTrust)
• Aircraft aerodynamic prediction method for V/STOL transition including flow separation (National Aeronautics and Space Administration, 1983), by B. R. Gilmer, D. R. Bristow, G. A. Miner, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Advanced prediction technique for the low speed aerodynamics of V/STOL aircraft (NASA Ames Research Center, 1983), by T. D. Beatty, M. K. Worthey, Vought Corporation, and Ames Research Center (page images at HathiTrust)
• V/STOL aircraft aerodynamic prediction methods investigation. Volume 2, Application of prediction methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by Peter T. Wooler, Henry Ziegler, Howard R. Wasson, Myles F. Schwendemann, H. C. |q Kao, Air Force Flight Dynamics Laboratory (U.S.), Northrop Corporation. Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• V/STOL aircraft aerodynamic prediction methods investigation. Volume 1, Theoretical development of prediction methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by Peter T. Wooler, Henry Ziegler, Howard R. Wasson, Myles F. Schwendemann, H. C. |q Kao, Air Force Flight Dynamics Laboratory (U.S.), Northrop Corporation. Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• An analysis of the stability and control characteristics of an ejector wing V/STOL during transition (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by George Kurylowich, James M. Martin, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Theoretical investigation of ducted propeller aerodynamics. Volume IV (Fort Eustis, Virginia : U.S. Army Transportation Research Command, 1961., 1961), by J. Sinacori, A. Lange, Republic Aviation Corporation, and United States. Army. Transportation Research Command (page images at HathiTrust)
• A general method for determining the aerodynamic characteristics of fan-in-wing configurations (Fort Eustis, Virginia : U.S. Army Aviation Materiel Laboratories, 1967., 1967), by U.S. Army Aviation Materiel Laboratories and Boeing Company. Commercial Airplane Division (page images at HathiTrust)
• V/STOL aircraft aerodynamic prediction methods investigation. Volume 3, Manual for computer programs (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by Peter T. Wooler, Henry Ziegler, Howard R. Wasson, Myles F. Schwendemann, H. C. |q Kao, Air Force Flight Dynamics Laboratory (U.S.), Northrop Corporation. Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)

• An investigation of a two-dimensional propulsive lifting system (National Aeronautics and Space Administration ;, 1973), by Carl A. Shollenberger, Ames Research Center, and California Institute of Technology (page images at HathiTrust)
• Rotorwash analysis handbook (Federal Aviation Administration, Research and Development Service ;, 1994), by Samuel W. Ferguson, Inc Systems Control Technology, EMA (Firm), and United States. Federal Aviation Administration. Research and Development Service (page images at HathiTrust)

• Aerodynamic characteristics of a vectored-thrust V/STOL fighter in the transition-speed range (National Aeronautics and Space Administration ;, 1973), by Raymond E. Mineck, Myles F. Schwendemann, and Langley Research Center (page images at HathiTrust)

• Proceedings of a Workshop on V/STOL Aircraft Aerodynamics (Monterey, Calif. : Dept. of the Navy, Naval Postgraduate School, [1979], 1979), by Workshop on V/STOL Aircraft Aerodynamics, M. F. Platzer, C. Henderson, and Naval Air Development Center (page images at HathiTrust; US access only)

• A compilation of the papers presented : Langley Research Center, Langley Field, Va., November 17-18, 1960. (National Aeronautics and Space Administration, 1960), by Va.) NASA Conference on V/STOL aircraft (1960 : Langley Field (page images at HathiTrust)
• Tactical uses of vertical lift aircraft : advanced paper[s], second annual technical symposium. (Headquarters USCONARC, 1967), by Close-the-Loop Operator-Engineer Technical Symposium (2nd : 1967) and American Helicopter Society (page images at HathiTrust)

• Thrust augmenting ejectors (Ames Research Center, 1979), by Workshop on Thrust Augmenting Ejectors (1978 : Ames Research Center), A. E. Lopez, Air Force Flight Dynamics Laboratory (U.S.), Naval Air Development Center, and Ames Research Center (page images at HathiTrust)

• NACA conference on some problems of aircraft operation; a compilation of the papers presented. (National Advisory Coimmittee for Aeronautics, 1950), by Lewis Flight Propulsion Laboratory NACA Conference on Some Problems of Aircraft Operation and Lewis Research Center (page images at HathiTrust)
• CAST-10-2/DOA 2 Airfoil Studies Workshop results : proceedings of a workshop (NASA, Office of Management, Scientific and Technical Information Division, 1989), by CAST-10-2/DOA 2 Airfoil Studies Workshop (1988 : NASA Langley Research Center), Acquilla S. Hill, and Edward J. Ray (page images at HathiTrust)
• Aeroelasticity symposium ... April 16-17, 1957. (National Aeronautics and Space Administration, 1963), by Germany) Aeroelastisches Kolloquim (1957 : Göttingen (page images at HathiTrust)
• Proceedings of the Circulation-Control Workshop 1986 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Circulation-Control Workshop (1986 : NASA Ames Research Center) and Jack Norman Nielsen (page images at HathiTrust)
• Advanced technology airfoil research. (National Aeronautics and Space Administration, 1979), by NASA Conference on Advanced Technology Airfoil Research (1978 : Langley Research Center) (page images at HathiTrust)

• Proceedings of the Third Symposium on the Plasma Sheath-Plasma Electromagnetics of Hypersonic Flight (Office of Aerospace Research, United States Air Force, 1967), by Symposium on the Plasma Sheath-Plasma Electromagnetics of Hypersonic Flight (3d : 1965 : Boston), Walter Rotman, and Air Force Cambridge Research Laboratories (U.S.). Microwave Physics Laboratory (page images at HathiTrust; US access only)
• Proceedings of Retardation and Recovery Symposium (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963, 1963), by Peter R. Murray, L. E. Winebrenner, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)

• Proceedings of the SCAR Conference, held at Langley Research Center, Hampton, Virginia, November, 9-12, 1976. (National Aeronautics and Space Administration ;, 1976), by Scar Conference (1976 : Langley Research Center) (page images at HathiTrust)
• Proceedings of the SCAR Conference, held at Langley Research Center, Hampton, Virginia, November, 9-12, 1976. -- (National Aeronautics and Space Administration ;, 1977), by Scar Conference (1976 : Langley Research Center) (page images at HathiTrust)
• YF-12 Experiments Symposium (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by YF-12 Experiments Symposium (1978 : Dryden Flight Research Center) and James and Associates (page images at HathiTrust)
• Proceedings of Retardation and Recovery Symposium (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963, 1963), by Peter R. Murray, L. E. Winebrenner, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)

• High Reynolds number research : a workshop (Scientific and Technical Information Office, National Aeronautics and Space Administration ;, 1977), by Va.)) Workshop on High Reynolds Number Research ((1st : : 1976 : : Hampton, Donald D. Baals, and Joint Institute for Advancement of Flight Sciences (page images at HathiTrust)
• Transonic Symposium: Theory, Application, and Experiment (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989), by Application Transonic Symposium: Theory, Jerome T. Foughner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic unsteady aerodynamics and aeroelasticity, 1987 : proceedings of a symposium sponsored by the National Aeronautics and Space Administration, Washington, D.C., and held at NASA Langley Research Center, Hampton, Virginia, May 20-22, 1987 (NASA, Scientific and Technical Information Division, 1989), by Samuel R. Bland, United States National Aeronautics and Space Administration, and Symposium on Transonic Unsteady Aerodynamics and Aeroelasticity (1987 : NASA Langley Research Center) (page images at HathiTrust)

• Aeroelasticity symposium ... April 16-17, 1957. (National Aeronautics and Space Administration, 1963), by Germany) Aeroelastisches Kolloquim (1957 : Göttingen (page images at HathiTrust)
• Proceedings. [David M. Jones, Symposium chairman] (Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962), by Ohio) Symposium on Aerothermoelasticity (1st : 1961 : Dayton, David M. Jones, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust; US access only)
• Proceedings of Symposium on Aeroelastic & Dynamic Modeling Technology, 23-24-25 September 1963, Dayton, Ohio (Defense Documentation Center], 1964), by Ohio) Symposium on Aeroelastic & Dynamic Modeling Technology (1963 : Dayton, William C. Nielsen, Aerospace Industries Association of America, and United States. Air Force. Systems Command. Research and Technology Division (page images at HathiTrust)
• Proceedings of Symposium on Aerothermoelasticity ; 30-31 October and 1 November 1961 (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, [1962], 1962), by David M. Jones and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Transonic unsteady aerodynamics and aeroelasticity, 1987 : proceedings of a symposium sponsored by the National Aeronautics and Space Administration, Washington, D.C., and held at NASA Langley Research Center, Hampton, Virginia, May 20-22, 1987 (NASA, Scientific and Technical Information Division, 1989), by Samuel R. Bland, United States National Aeronautics and Space Administration, and Symposium on Transonic Unsteady Aerodynamics and Aeroelasticity (1987 : NASA Langley Research Center) (page images at HathiTrust)

• Numerical boundary condition procedures : proceedings of a symposium held at NASA Ames Research Center, Moffett Field, California, October 19-20, 1981. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Ames Research Center, and Symposium on Numerical Boundary Condition Procedures (1981 : NASA Ames Research Center) (page images at HathiTrust)

• Proceedings of Retardation and Recovery Symposium (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963, 1963), by Peter R. Murray, L. E. Winebrenner, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)

• Supersonic symposium : the men of Mach 1 (Air Force Flight Test Center History Office, 1990), by Calif.) Supersonic Symposium (1987 : Edwards Air Force Base and James O. Young (page images at HathiTrust)

More items available under broader and related terms at left.